Thermal spray powders for wear-resistant coatings, and related methods
Abstract
A method of making a thermal spray powder is provided. The method comprises: providing a powder comprising a plurality of porous particles; infiltrating a mixture comprising a solvent and a plurality of solid lubricant particles into the porous particles; and heating the powder to a temperature sufficient to evaporate the solvent. The method of forming a wear-resistant coating is provided. The method comprises: providing a thermal spray powder; heating the thermal spray powder; and accelerating the thermal spray powder from a thermal spray gun onto the substrate, to form a deposit. Yet another embodiment provides a wear resistant coating. The wear resistant coating is formed by thermally spraying the thermal spray powder.
Claims
exact text as granted — not AI-modified1 . A method of making a thermal spray powder, the method comprising:
providing a powder comprising a plurality of porous particles; infiltrating a mixture comprising a solvent and a plurality of solid lubricant particles into the porous particles, and heat-treating the powder to a temperature sufficient to evaporate the solvent.
2 . The method of claim 1 , wherein the porous particles comprise a material selected from the group consisting of a metal, a metal alloy, a ceramic, a cermet, and combinations thereof.
3 . The method of claim 2 , wherein the metal comprises at least one metal selected from the group consisting of titanium, nickel, iron, cobalt, chromium, aluminum, and yttrium.
4 . The method of claim 2 , wherein the ceramic comprises a material selected from the group consisting of aluminum oxide, chromium oxide, chromium-carbide, tantalum carbide, titanium diboride, titanium oxide, tungsten-carbide, and titanium carbide.
5 . The method of claim 2 , wherein the cermet comprises a material selected from the group consisting of tungsten carbide-cobalt, nickel aluminide, nickel chrome-chrome carbide, and tungsten carbide-cobalt chrome.
6 . The method of claim 5 , wherein the cermet comprises a material selected from the group consisting of tungsten carbide-cobalt and tungsten carbide-cobalt chrome.
7 . The method of claim 1 , wherein the porous particles have an average pore size in the range from about 1 micrometer to about 10 micrometers.
8 . The method of claim 7 , wherein the porous particles have an average pore size in the range from about 1 micrometer to about 5 micrometers.
9 . The method of claim 1 , wherein the porous particles have a porosity in a range of from about 1% to about 90%.
10 . The method of claim 1 , wherein the solid lubricant particles comprise at least one material selected from the group consisting of a fluoride, a nitride, a sulfide, carbon, and boric acid.
11 . The method of claim 10 , wherein the solid lubricant particles comprise at least one material selected from the group consisting of hexagonal boron nitride, graphite, molybdenum disulfide, tungsten sulfide, calcium difluoride, calcium-barium difluoride, polytetrafluoroethylene, carbon, and boric acid.
12 . The method of claim 10 , wherein the solid lubricant particles comprise hexagonal boron nitride.
13 . The method of claim 1 , wherein the solid lubricant particles have an average particle size less than about 5 micrometers.
14 . The method of claim 13 , wherein the solid lubricant particles have an average particle size in the range from about 20 nanometers to about 3 micrometers.
15 . The method of claim 1 , wherein the solvent comprises a material selected from the group consisting of water, acetone, and alcohol.
16 . The method of claim 15 , wherein the solvent comprises water.
17 . The method of claim 1 , wherein infiltration comprises at least one process selected from the group consisting of injection, vacuum infiltration, and capillary filling of the solution.
18 . The method of claim 17 , wherein infiltration comprises vacuum-infiltration.
19 . The method of claim 18 , wherein the vacuum infiltration comprises contacting the porous particle with the solution at a pressure of at least about −1.0 bar.
20 . The method of claim 1 , wherein heat-treating comprises heating to a temperature in a range from about 20° C. to about 250° C.
21 . The method of claim 1 , wherein the thermal spray powder comprises the solid lubricant particles in an amount of at least about 5 volume percent.
22 . The method of claim 1 , wherein the thermal spray powder comprises the solid lubricant in an amount in a range of about 5 volume percent to about 80 volume percent.
23 . A method of making a thermal spray powder, the method comprising:
providing a powder which comprises porous particles of cobalt tungsten carbide; vacuum-infiltrating a mixture comprising water and hexagonal boron nitride into the porous particles, and heat-treating the powder to a temperature sufficient to evaporate the solvent.
24 . A method of forming a wear-resistant coating on a substrate, the method comprising:
providing a thermal spray powder; heating the thermal spray powder; and accelerating the thermal spray powder from a thermal spray gun onto the substrate, to form a deposit, wherein the thermal spray powder is formed by the process of: providing a powder comprising a plurality of porous particles; infiltrating a mixture comprising a solvent and a plurality of solid lubricant particles into the porous particles, and heat-treating the powder to a temperature sufficient to evaporate the solvent.
25 . The method of claim 24 , wherein the porous particles comprise a material selected from the group consisting of a metal, a metal alloy, a ceramic, a cermet, and combinations thereof.
26 . The method of claim 24 , wherein the solid lubricant particles comprise at least one material selected from the group consisting of hexagonal boron nitride, graphite, molybdenum disulfide, tungsten sulfide, calcium difluoride, calcium-barium difluoride, polytetrafluoroethylene, carbon, and boric acid.
27 . A wear-resistant coating formed by the method of claim 24 .
28 . A turbomachine containing at least one surface covered by the wear-resistant coating of claim 27 .Cited by (0)
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